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MIL-A-83377 Revision B:1978

Superseded

Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

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superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

ADHESIVE BONDING (STRUCTURAL) FOR AEROSPACE AND OTHER SYSTEMS, REQUIREMENTS FOR

Available format(s)

PDF

Superseded date

12-31-1997

1. SCOPE
2. APPLICABLE DOCUMENTS
3. REQUIREMENTS
4. QUALITY ASSURANCE PROVISIONS
5. PACKAGING
6. NOTES

Prerequisites for structural adhesive bonding of metal, core material and composites.

Committee
FSC 8040
DevelopmentNote
B NOTICE 1 - Notice of Validation. B NOTICE 2 - Notice of Cancellation without replacement. (06/2004)
DocumentType
Standard
Pages
19
PublisherName
US Military Specs/Standards/Handbooks
Status
Superseded
SupersededBy

MIL-HDBK-337 Base Document:1982 ADHESIVE BONDED AEROSPACE STRUCTURE REPAIR
MIL-A-85705 Revision A:1987 ADHESIVE, AIRCRAFT, FOR STRUCTURAL REPAIR
DEFSTAN 00-970(PT7)SEC4/2(2007) : 2007 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 4: DETAIL DESIGN AND STRENGTH OF MATERIALS
DEFSTAN 00-970(PT0)/9(2012) : 2012 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
MIL-HDBK-1587 Base Document:1996 MATERIALS AND PROCESS REQUIREMENTS FOR AIR FORCE WEAPON SYSTEM
DEFSTAN 00-970(PT0)/14(2014) : 2014 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
DEFSTAN 00-970(PT0)/7(2011) : 2011 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
DEFSTAN 00-970(PT0)/13(2014) : 2014 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
DEFSTAN 00-970(PT0)/12(2014) : 2014 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
DEFSTAN 00-970(PT0)/11(2013) : 2013 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
DEFSTAN 00-970(PT0)/8(2011) : 2011 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
DEFSTAN 00-970(PT0)/10(2013) : 2013 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
DEFSTAN 00-970(PT7)SEC2/SUPP4/5(2015) : INTERIM DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SUPPLEMENT 4: DESIGN AND CONSTRUCTION (SUBPART D)
DEFSTAN 00-970(PT7)SEC2/SUPP4/6(2015) : 2015 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SUPPLEMENT 4: DESIGN AND CONSTRUCTION (SUBPART D)
MIL-F-7179 Revision G:1993 FINISHES, COATINGS, AND SEALANTS FOR THE PROTECTION OF AEROSPACE WEAPONS SYSTEM
MIL-R-85880 Base Document:1988 ROCKET, JET ASSISTED TAKE OFF (JATO) PROPULSION SYSTEM, GENERAL DEVELOPMENT SPECIFICATION FOR
MIL-STD-1547 Revision B:1992 ELECTRONIC PARTS, MATERIALS, AND PROCESSES FOR SPACE VEHICLES
MIL-HDBK-349 Base Document:1994 MANUFACTURE AND INSPECTION OF ADHESIVE BONDED, ALUMINUM HONEYCOMB SANDWICH ASSEMBLIES FOR AIRCRAFT
MIL-R-7705 Revision B:1975 RADOME, GENERAL SPECIFICATION FOR
IPC HDBK 630 : 0 GUIDELINES FOR DESIGN, MANUFACTURE, INSPECTION AND TESTING OF ELECTRONIC ENCLOSURES ASSEMBLY
MIL-I-85889 Base Document:1988 IGNITER, JET ASSISTED TAKE OFF (JATO) PROPULSION SYSTEM, GENERAL DEVELOPMENT SPECIFICATION FOR
SAE AMS 3109 : 2014 PRIMER, ADHESIVE, ELECTRODEPOSITED -55 TO +82 DEGREES C (-67 TO +180 DEGREES F)
MIL-A-25463 Revision B:1982 ADHESIVE, FILM FORM, METALLIC STRUCTURAL SANDWICH CONSTRUCTION
DEFSTAN 00-970(PT7)SEC4/1(2006) : 2006 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 4: DETAIL DESIGN AND STRENGTH OF MATERIALS
MIL-A-83376 Revision A:1978 ADHESIVE BONDED METAL FACED, SANDWICH STRUCTURES, ACCEPTANCE CRITERIA
ADS-13F-HDBK : 1997 AERONAUTICAL DESIGN STANDARD - HANDBOOK - AIR VEHICLE MATERIALS AND PROCESSES
SAE AMS A 25463 : 2013 ADHESIVE, FILM FORM, METALLIC STRUCTURAL SANDWICH CONSTRUCTION
MIL-I-83456 Base Document:1974 INSTALLATION OF SEGMENTED LIGHTNING DIVERTER STRIPS ON AIRCRAFT RADOMES, GENERAL SPECIFICATION FOR
MIL-P-9400 Revision C:1991 PLASTIC LAMINATE AND SANDWICH CONSTRUCTION PARTS, AIRCRAFT STRUCTURAL PROCESS SPECIFICATION REQUIREMENTS

MIL I 6870 : E INSPECTION PROGRAM REQUIREMENTS NONDESTRUCTIVE FOR AIRCRAFT AND MISSILE MATERIALS AND PARTS
MIL-A-83376 Revision A:1978 ADHESIVE BONDED METAL FACED, SANDWICH STRUCTURES, ACCEPTANCE CRITERIA
MIL C 5541 : E CHEMICAL CONVERSION COATINGS ON ALUMINUM AND ALUMINUM ALLOYS
MIL A 8625 : F ANODIC COATINGS FOR ALUMINUM AND ALUMINUM ALLOYS
UU-P-268 Revision G:1973 PAPER, KRAFT, WRAPPING
SAE ARP 1524 : 2013 SURFACE PREPARATION AND PRIMING OF ALUMINUM ALLOY PARTS FOR HIGH DURABILITY STRUCTURAL ADHESIVE BONDING

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